US8931508B2 - Piloted fuel tank vapor isolation valve - Google Patents

Piloted fuel tank vapor isolation valve Download PDF

Info

Publication number
US8931508B2
US8931508B2 US12/542,207 US54220709A US8931508B2 US 8931508 B2 US8931508 B2 US 8931508B2 US 54220709 A US54220709 A US 54220709A US 8931508 B2 US8931508 B2 US 8931508B2
Authority
US
United States
Prior art keywords
chamber
valve
vapor
pilot
stage
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related, expires
Application number
US12/542,207
Other languages
English (en)
Other versions
US20100051116A1 (en
Inventor
Charles J. Martin
Matthew L. Erdmann
James P. Ostrosky
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Eaton Corp
Original Assignee
Eaton Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Eaton Corp filed Critical Eaton Corp
Priority to US12/542,207 priority Critical patent/US8931508B2/en
Assigned to EATON CORPORATION reassignment EATON CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MARTIN, CHARLES J., ERDMANN, MATTHEW L., OSTROSKY, JAMES P.
Publication of US20100051116A1 publication Critical patent/US20100051116A1/en
Application granted granted Critical
Publication of US8931508B2 publication Critical patent/US8931508B2/en
Expired - Fee Related legal-status Critical Current
Adjusted expiration legal-status Critical

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
    • F02M25/08—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding fuel vapours drawn from engine fuel reservoir
    • F02M25/0836—Arrangement of valves controlling the admission of fuel vapour to an engine, e.g. valve being disposed between fuel tank or absorption canister and intake manifold
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
    • F02M25/08—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding fuel vapours drawn from engine fuel reservoir
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00—Actuating devices; Operating means; Releasing devices
    • F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
    • F16K31/126—Actuating devices; Operating means; Releasing devices actuated by fluid the fluid acting on a diaphragm, bellows, or the like
    • F16K31/1262—Actuating devices; Operating means; Releasing devices actuated by fluid the fluid acting on a diaphragm, bellows, or the like one side of the diaphragm being spring loaded
    • F16K31/1264—Actuating devices; Operating means; Releasing devices actuated by fluid the fluid acting on a diaphragm, bellows, or the like one side of the diaphragm being spring loaded with means to allow the side on which the springs are positioned to be altered
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00—Actuating devices; Operating means; Releasing devices
    • F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
    • F16K31/126—Actuating devices; Operating means; Releasing devices actuated by fluid the fluid acting on a diaphragm, bellows, or the like
    • F16K31/128—Actuating devices; Operating means; Releasing devices actuated by fluid the fluid acting on a diaphragm, bellows, or the like servo actuated
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00—Actuating devices; Operating means; Releasing devices
    • F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
    • F16K31/36—Actuating devices; Operating means; Releasing devices actuated by fluid in which fluid from the circuit is constantly supplied to the fluid motor
    • F16K31/38—Actuating devices; Operating means; Releasing devices actuated by fluid in which fluid from the circuit is constantly supplied to the fluid motor in which the fluid works directly on both sides of the fluid motor, one side being connected by means of a restricted passage and the motor being actuated by operating a discharge from that side
    • F16K31/385—Actuating devices; Operating means; Releasing devices actuated by fluid in which fluid from the circuit is constantly supplied to the fluid motor in which the fluid works directly on both sides of the fluid motor, one side being connected by means of a restricted passage and the motor being actuated by operating a discharge from that side the fluid acting on a diaphragm
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00—Actuating devices; Operating means; Releasing devices
    • F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
    • F16K31/36—Actuating devices; Operating means; Releasing devices actuated by fluid in which fluid from the circuit is constantly supplied to the fluid motor
    • F16K31/40—Actuating devices; Operating means; Releasing devices actuated by fluid in which fluid from the circuit is constantly supplied to the fluid motor with electrically-actuated member in the discharge of the motor
    • F16K31/402—Actuating devices; Operating means; Releasing devices actuated by fluid in which fluid from the circuit is constantly supplied to the fluid motor with electrically-actuated member in the discharge of the motor acting on a diaphragm
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K7/00—Diaphragm valves or cut-off apparatus, e.g. with a member deformed, but not moved bodily, to close the passage ; Pinch valves
    • F16K7/12—Diaphragm valves or cut-off apparatus, e.g. with a member deformed, but not moved bodily, to close the passage ; Pinch valves with flat, dished, or bowl-shaped diaphragm
    • F16K7/14—Diaphragm valves or cut-off apparatus, e.g. with a member deformed, but not moved bodily, to close the passage ; Pinch valves with flat, dished, or bowl-shaped diaphragm arranged to be deformed against a flat seat
    • F16K7/17—Diaphragm valves or cut-off apparatus, e.g. with a member deformed, but not moved bodily, to close the passage ; Pinch valves with flat, dished, or bowl-shaped diaphragm arranged to be deformed against a flat seat the diaphragm being actuated by fluid pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K15/00—Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
    • B60K15/03—Fuel tanks
    • B60K15/035—Fuel tanks characterised by venting means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K15/00—Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
    • B60K15/03—Fuel tanks
    • B60K2015/0321—Fuel tanks characterised by special sensors, the mounting thereof
    • B60K2015/03217—Fuel level sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K15/00—Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
    • B60K15/03—Fuel tanks
    • B60K15/035—Fuel tanks characterised by venting means
    • B60K2015/03561—Venting means working at specific times
    • B60K2015/03576—Venting during filling the reservoir
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
    • F02M25/08—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding fuel vapours drawn from engine fuel reservoir
    • F02M25/089—Layout of the fuel vapour installation
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7287—Liquid level responsive or maintaining systems
    • Y10T137/7329—With supplemental or safety closing means or bias
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7758—Pilot or servo controlled
    • Y10T137/7761—Electrically actuated valve
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7758—Pilot or servo controlled
    • Y10T137/7762—Fluid pressure type
    • Y10T137/7764—Choked or throttled pressure type
    • Y10T137/7766—Choked passage through main valve head
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7758—Pilot or servo controlled
    • Y10T137/7762—Fluid pressure type
    • Y10T137/7769—Single acting fluid servo
    • Y10T137/777—Spring biased
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/8593—Systems
    • Y10T137/87265—Dividing into parallel flow paths with recombining
    • Y10T137/8733—Fluid pressure regulator in at least one branch
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/8593—Systems
    • Y10T137/87265—Dividing into parallel flow paths with recombining
    • Y10T137/87338—Flow passage with bypass
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/8593—Systems
    • Y10T137/87265—Dividing into parallel flow paths with recombining
    • Y10T137/87499—Fluid actuated or retarded
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/8593—Systems
    • Y10T137/87265—Dividing into parallel flow paths with recombining
    • Y10T137/87555—Having direct response valve [e.g., check valve, etc.]

Definitions

  • This disclosure relates to isolation valves useful in, among other things, fuel tank vapor control systems.
  • Fuel tank vapor and emission control systems may be used to control the flow of fuel vapors from a vehicle's fuel tank and also to control the relative pressure of the fuel tank. Vapors may be vented to a canister or other similar vapor control structure where hydrocarbon vapors are stored and which is also connected to the engine air inlet.
  • Fuel tanks may generate fuel vapors during various operating phases and these vapors may be directed to a canister or other component responsible for storing them, and then purging them regularly to the admission header of the engine. Periodic purging of stored vapors may be necessary during operation of the vehicle. To conduct the purge, the fuel system is operated to control flow of vapor from the storage canister to the engine air inlet, and atmospheric air is admitted to purge the canister.
  • a vapor isolation valve for a fuel tank includes a first chamber in fluid communication with the fuel tank and a second chamber adjacent to the first chamber.
  • a diaphragm is disposed between the first and second chambers and has a diaphragm orifice allowing fluid communication between the first and second chambers.
  • the diaphragm is moveable between a diaphragm open position and a diaphragm closed position.
  • a third chamber is disposed on the same side of the diaphragm as the first chamber and is in fluid communication with an exit passage.
  • the diaphragm open position allows fluid communication between the first chamber and the third chamber, and the diaphragm closed position substantially restricts fluid communication between the first chamber and the third chamber.
  • a pilot valve is disposed between the second and third chambers and is selectively moveable between a pilot open position configured to allow fluid communication between the second and third chambers and a pilot closed position configured to block fluid communication between the second and third chambers.
  • the vapor isolation valve may be in communication with a control system, and the pilot valve configured to move between the pilot open and closed positions in response to an electronic signal from the control system.
  • FIG. 1 is a schematic diagram of a vapor isolation valve in a steady state condition, in which there is substantially no flow or venting occurring;
  • FIG. 2 is a schematic diagram of the vapor isolation valve in a low flow state, in which vapors are venting to an exit passage through a pilot valve;
  • FIG. 3 is a schematic diagram of the vapor isolation valve in a high flow state, in which vapors are venting to an exit passage;
  • FIG. 4 is a schematic diagram of the vapor isolation valve in a restricted flow state, in which vapors are venting to an exit passage and pressures are limited by a restrictor plate;
  • FIG. 5 is a schematic diagram of the vapor isolation valve in a pressure-relief state, in which vapors are venting to an exit passage via a pressure relief valve and there is substantially no flow through the valve chambers.
  • FIG. 1 an embodiment of a vapor isolation valve 10 .
  • the valve 10 controls transfer of fuel vapors, air, and other fluids between a fuel tank 12 (represented schematically below the valve 10 ) and an exit passage 14 .
  • the valve 10 may be located or mounted directly on the fuel tank 12 or may be mounted remotely. Additional components, such as, without limitation, additional valves (not shown) or passageways (not shown) may be interspersed between the fuel tank 12 and the valve 10 . Exit passage 14 may be in communication with the vehicle's evaporative system (not shown) and may also be referred to as the vent path, as this is the path for venting or relieving excess fuel vapor from the fuel tank 12 .
  • Valve 10 includes three main primary chambers.
  • a first chamber 16 is in fluid communication with the fuel tank 12 , either directly or via additional passageways and valves.
  • a second chamber 18 is disposed above (as viewed in FIG. 1 ) the first chamber 16 , and a third chamber 20 is in fluid communication with the exit passage 14 .
  • a diaphragm 24 is disposed between the first chamber 16 and the second chamber 18 , and also between the third chamber 20 and the second chamber 18 .
  • the diaphragm 24 has a diaphragm orifice 26 , which allows limited fluid communication—because the diaphragm orifice 26 is relatively small—between the first chamber 16 and the second chamber 18 .
  • the diaphragm 24 is moveable between a diaphragm closed position (shown schematically in FIGS. 1 , 2 and 5 ) and a diaphragm open position (shown schematically in FIGS. 3 and 4 , and discussed in more detail herein).
  • the diaphragm 24 may be referred to as a membrane or membrane valve, and may be formed from a compliant material, such as, without limitation: natural rubber, synthetic rubber, silicone, or another material as would be recognized by a person having ordinary skill in the art. Diaphragm 24 may further include a steel or a plastic portion, through which the diaphragm orifice 26 may be formed, as long as the diaphragm 24 is movable between the diaphragm open position and the diaphragm closed position.
  • a compliant material such as, without limitation: natural rubber, synthetic rubber, silicone, or another material as would be recognized by a person having ordinary skill in the art.
  • Diaphragm 24 may further include a steel or a plastic portion, through which the diaphragm orifice 26 may be formed, as long as the diaphragm 24 is movable between the diaphragm open position and the diaphragm closed position.
  • the third chamber 20 is disposed on the same side of the diaphragm 24 as the first chamber 16 . Therefore, the diaphragm open position allows fluid communication between the first chamber 16 and the third chamber 20 and the diaphragm closed position substantially restricts fluid communication between the first chamber 16 and the third chamber 20 .
  • the fuel vapors within the first chamber 16 have a first surface area or effective contact area with the diaphragm 24 and the second chamber 18 has a second area in contact with the diaphragm 24 .
  • Vapor within the third chamber 20 has a third surface area with the diaphragm 24 .
  • the second surface area is larger than the third surface area
  • the third surface area is larger than the first surface area. Note, however, that the third chamber 20 need not surround the first chamber 16 , as shown in FIG. 1 , but may be adjacent to the first chamber 16 .
  • the valve 10 also includes a pilot valve 30 that is disposed between the second chamber 18 and the third chamber 20 .
  • the pilot valve 30 is selectively moveable between a pilot open position (shown schematically in FIGS. 2-4 and discussed in more detail herein) and a pilot closed position (shown schematically in FIGS. 1 and 5 ).
  • the pilot open position is configured to allow fluid communication between the second chamber 18 and the third chamber 20
  • the pilot closed position is configured to block fluid communication between the second chamber 18 and the third chamber 20 .
  • the valve 10 is in communication with a control system 32 .
  • the pilot valve 30 is configured to move between the pilot open position and the pilot closed position in response to an electronic signal from the control system 32 .
  • the control system 32 may be, without limitation, an engine electronic control (EEC), powertrain control module (PCM), engine control unit (ECU), or other structure suitable to control the pilot valve 30 and valve 10 .
  • the valve 10 includes the pilot valve 30 and the opening and closing characteristics of the valve 10 are controlled or operated by the control system 32 , and may, therefore, also be referred to as a Piloted Fuel Tank Vapor Isolation Valve (PVIV).
  • the PVIV valve 10 may be used to regulate fuel vapors exiting the fuel tank 12 .
  • valve 10 may have additional operating conditions or configurations within the scope of the appended claims.
  • the pressure within the first, second, and third chambers, 16 , 18 , and 20 are referred to herein as P 1 , P 2 , and P 3 , respectively.
  • P 1 , P 2 , and P 3 are referred to herein as P 1 , P 2 , and P 3 , respectively.
  • P 3 the pressure within the third chamber 20
  • the operating condition shown may be referred to as a normal operating condition or a run-loss condition. This condition may occur when a vehicle is being operated and conditions have generated some fuel vapor, but the control strategy is to contain that vapor.
  • the control system 32 places the pilot valve 30 in the pilot closed position—which may be its normal or default state—and the fuel tank 12 is therefore at a positive pressure relative to the exit passage 14 . Therefore, the pressure in the first chamber 16 is greater than the pressure in the third chamber 20 ; P 1 >P 3 .
  • the diaphragm orifice 26 that connects the first chamber 16 to the second chamber 18 keeps P 1 and P 2 at equilibrium, and both are greater than P 3 .
  • P 1 and P 2 are at the same pressure
  • the diaphragm 24 remains in the diaphragm closed position and sealed against vapor flow between the first and third chambers 16 and 20 .
  • the diaphragm 24 seals against flow of vapor because P 3 is lower than P 1 and P 2 , so there is a net force downward (as viewed in the figures) on the diaphragm 24 due to the second chamber 18 allowing P 2 to be applied over a larger area, the second surface area. There is no vapor flow in this scenario.
  • the vehicle programming may determine that venting of the fuel tank 12 is desired during normal vehicle operation.
  • the control system 32 will then instruct the pilot valve 30 to switch or move to the pilot open position by sending an electronic signal to the pilot valve 30 .
  • P 1 will initially be the same as P 2 —because, as described above, pressure is equalized due to the diaphragm orifice 26 —and P 2 is greater than P 3 .
  • valve 10 may further include a diaphragm spring 34 , which is configured to bias the diaphragm toward the first chamber 16 and the diaphragm closed position.
  • the combined downward spring force (as viewed in FIGS. 1 and 2 ) of the diaphragm spring 34 and the diaphragm 24 itself will maintain the diaphragm 24 in the diaphragm closed position and continue to seal against flow directly between the first chamber 16 and the third chamber 20 . Therefore, the through the exit passage 14 will occur at a first exit flow rate, which is a relatively low flow. This low flow rate is shown schematically in FIG. 2 as small flow arrow 50 .
  • the flow path through the pilot valve 30 may be sized much larger than the flow path through the diaphragm orifice 26 .
  • the valve 10 therefore acts as a two-stage exit flow mechanism when venting high pressure from the fuel tank 12 to the exit passage 14 .
  • the two-stage exit flow may reduce wear on the valve 10 and the remainder of the fuel system by damping transitions between no vapor flow and high vapor flow.
  • the two-stage flow may reduce the pressure differentials across other valves—such as, without limitation, fill/fuel level vapor valves (FLVV) or grade vent valves (GVV)—which are located between the fuel tank 12 and the valve 10 . Reducing the pressure differential across, for example, an FLVV reduces the likelihood that the FLVV valve will be improperly closed due to corking. “Corking” is a phenomenon where the force of the rushing fuel vapors may physically lift the valve float up against the seat, thereby blocking free vapor exit through the valve.
  • the diaphragm spring 34 may be combined with a metal or plastic disc slidably disposed between the first and third chambers 16 , 20 and the second chamber 18 . Such a configuration may replace the compliant-material based diaphragm 24 by allowing the disc to move or slide between the diaphragm open and closed positions without flexing. In such a configuration, the spring force would be generated from substantially only the diaphragm spring 34 .
  • valve 10 For refueling, pressure in the fuel tank 12 needs to be relieved before the cap is opened and the fuel-fill event begun. This is also referred to as venting the fuel tank 12 prior to refueling.
  • the valve 10 will initially be in a steady-state, such that P 1 will be equal to P 2 , and P 3 will be at a lower pressure; as shown in FIG. 1 .
  • the pilot valve 30 When the control system 32 recognizes a fuel-fill event is about to occur, the pilot valve 30 is switched to the pilot open position and the vapor in the second chamber 18 (above the diaphragm 24 ) will begin to dump through the pilot valve 30 to the third chamber 20 and exit passage 14 ; as shown in FIG. 2 . Once sufficient pressure is relieved from the second chamber 18 , the diaphragm 24 will deflect to the diaphragm open position. The diaphragm open position will allow high flow from the valve 10 ; as shown in FIG. 3 .
  • the fuel-fill event completes when the fuel tank 12 becomes full, e.g. when a fuel level within fuel tank 12 reaches a predetermined level.
  • the vehicle may include an in-tank fuel sender 36 or a pressure transducer 38 (or both).
  • the pressure transducer 38 may not directly monitor the fuel level, but determines the pressure within fuel tank 12 . It is possible to tell when the fuel tank 12 is full at the end of the fuel-fill event because the pressure will spike.
  • the in-tank fuel sender 36 and pressure transducer 38 may also be used for other purposes, such as signaling the vehicle operator of the fuel level via the gas gauge or monitoring pressure levels within the fuel tank 12 .
  • the control system 32 is in communication with either the in-tank fuel sender 36 or the pressure transducer 38 , and is configured to monitor the fuel level during fuel-fill events. As the fuel level nears or reaches the full level (or some other predetermined fuel level) the pilot valve 30 moves to the pilot closed position in response to an electronic signal indicating completion of the fuel-fill event.
  • the electronic signal indicating completion of the fuel-fill event may be generated by either the in-tank fuel sender 36 or the pressure transducer 38 and may be sent directly to the control system 32 or filtered through other components.
  • valve 10 may include a restrictor plate 42 , which is disposed between the first chamber 16 and the fuel tank 12 .
  • the restrictor plate 42 limits the flow rate of vapors between the fuel tank 12 and the first chamber 16 , and therefore causes a pressure differential between the fuel tank 12 and the first chamber 16 .
  • the pressure differential is illustrated schematically in FIG. 4 as large and small arrows (shown in phantom), below and above the restrictor plate 42 , respectively. Usage of the restrictor plate 42 is dependant on the pressure difference across the additional valves (FLVV or GVV) during venting of the fuel tank 12 , just prior to fuel-fill event. If the pressure difference is high, the probability of valve corking is also high, and usage of the restrictor plate 42 would be recommended.
  • Restrictor plate 42 usage is dependant on system architecture—such as fuel tank 12 pressure relief points and valve (FLVV) orifice diameter.
  • a restrictor spring 44 may also be included, and is configured to bias the restrictor plate 42 toward the fuel tank 12 .
  • Pressure differentials or changes in the relative pressures of the fuel tank 12 and exit passage 14 may occur while the vehicle is parked or otherwise not operating. Pressure equalization of P 1 and P 2 occurs via the diaphragm orifice 26 in the diaphragm 24 . If there is any vapor generation in the fuel tank 12 , P 1 and P 2 will be larger than P 3 . As the pilot valve 30 is closed and the pressure of P 1 and P 2 are equal on either side of the diaphragm, vapor will be contained within the fuel tank 12 .
  • P 3 is larger than both P 1 and P 2 . This event could occur either during vehicle operation or parking conditions. This could represent a condition where the vehicle is parked overnight in a hot environment, and it is possible that a vacuum could be formed in the fuel tank 12 during overnight cooling of the fuel tank 12 . With the pilot valve 30 closed, unless the pressure P 3 becomes large enough to override the effect of the spring force, pressure equalization of the fuel tank 12 will not occur.
  • pressure in the fuel tank 12 may reach levels that could compromise the integrity of the fuel system. To prevent this from happening, there are several possible configurations.
  • the pressure transducer 38 may be used. This pressure transducer 38 could be integrated into the PVIV valve 10 or anywhere else in the fuel system that is exposed to the fuel tank 12 and capable of monitoring the vapor pressure therein.
  • the control system 32 can activate the pilot valve 30 , switching it to the pilot open position. Opening the pilot valve 30 allows pressure P 2 (above the diaphragm 24 ) to bleed off and venting to occur in the same manner during the refueling—first at the low flow rate shown in FIG. 2 and then the high flow rate shown in FIG. 3 , if necessary.
  • valve 10 is shown accomplishing pressure relief through the use of mechanical structure not requiring actuation from the control system 32 . This is shown schematically in FIG. 5 as pressure relief flow 54 .
  • the valve 10 may further include a pressure relief valve 46 .
  • a bypass channel 48 places the pressure relief valve 46 in fluid communication with the fuel tank 12 and the exit passage 14 .
  • the pressure relief valve 46 is configured to selectively allow vapor flow from the fuel tank 12 to the exit passage 14 when the pressure differential between the fuel tank 12 and the exit passage 14 reaches a predetermined threshold. Because the pressure relief valve 46 operates solely on pressure differentials, this pressure relief flow 54 may occur when the pilot valve 30 is in either of the pilot open and pilot closed positions.
  • a dead weight head valve ball or disc over an orifice
  • a spring-loaded valve may be utilized.
  • the pressure relief valve 46 may be packaged within the PVIV valve 10 , as part of the pilot valve 30 , or elsewhere in the system.
  • the PVIV valve 46 contains structure capable of relieving the fuel tank 12 without interaction from the control system 12 .
  • the PVIV valve 10 may be installed on vehicles equipped for on-board diagnostics (OBD). For OBD to occur, a vacuum is pulled from the engine intake manifold, which is in fluid communication with the exit passage 14 , and the vehicle controls test for leaks in the fuel system.
  • the fuel tank 12 is generally included in the components of the fuel system which need to be leak-checked during the OBD process.
  • the exit passage 14 is purposefully lowered below atmospheric pressure.
  • the control system 32 places the pilot valve 30 in the pilot open position. Because flow through the valve 10 is generated based upon pressure differentials between the first, second, and third chambers 16 , 18 , and 20 , operation of the valve 10 remains substantially the same even though the exit passage 14 is well below atmospheric pressure in this situation.
  • P 2 will become equal to P 3 due to low flow through the pilot valve 30 (as shown in FIG. 2 ), and P 2 and P 3 will be less than P 1 . Because P 2 acts on the second surface area, which is a larger area than the third surface area over which P 3 acts, the diaphragm 24 will open and communication between the exit passage 14 the fuel tank 12 will exist, allowing the OBD leak check to occur.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Transportation (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Supplying Secondary Fuel Or The Like To Fuel, Air Or Fuel-Air Mixtures (AREA)
  • Fluid-Driven Valves (AREA)
US12/542,207 2008-08-26 2009-08-17 Piloted fuel tank vapor isolation valve Expired - Fee Related US8931508B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US12/542,207 US8931508B2 (en) 2008-08-26 2009-08-17 Piloted fuel tank vapor isolation valve

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US9179508P 2008-08-26 2008-08-26
US12/542,207 US8931508B2 (en) 2008-08-26 2009-08-17 Piloted fuel tank vapor isolation valve

Publications (2)

Publication Number Publication Date
US20100051116A1 US20100051116A1 (en) 2010-03-04
US8931508B2 true US8931508B2 (en) 2015-01-13

Family

ID=41323480

Family Applications (1)

Application Number Title Priority Date Filing Date
US12/542,207 Expired - Fee Related US8931508B2 (en) 2008-08-26 2009-08-17 Piloted fuel tank vapor isolation valve

Country Status (9)

Country Link
US (1) US8931508B2 (ja)
EP (1) EP2321518B1 (ja)
JP (2) JP2012500750A (ja)
KR (1) KR101602981B1 (ja)
CN (1) CN102165174B (ja)
AU (1) AU2009286409A1 (ja)
MX (1) MX2011002245A (ja)
RU (1) RU2011111497A (ja)
WO (1) WO2010023534A1 (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170253116A1 (en) * 2012-12-24 2017-09-07 Eaton Corporation Valve assembly for a tank of a vehicle and a method of creating a vacuum in the tank

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011015999B4 (de) 2011-04-04 2015-06-25 Audi Ag Verfahren zum Entlüften eines Kraftstofftanks eines Fahrzeugs und Tankentlüftungsvorrichtung
JPWO2013018215A1 (ja) * 2011-08-03 2015-03-02 トヨタ自動車株式会社 燃料タンクシステム
JP5807527B2 (ja) * 2011-12-01 2015-11-10 トヨタ自動車株式会社 燃料タンクシステム
JP5724883B2 (ja) * 2012-01-10 2015-05-27 トヨタ自動車株式会社 燃料タンクシステム
JP5849713B2 (ja) * 2012-01-13 2016-02-03 トヨタ自動車株式会社 燃料タンクシステム
JP5810942B2 (ja) * 2012-01-27 2015-11-11 トヨタ自動車株式会社 燃料タンクシステム
JP5821683B2 (ja) * 2012-02-21 2015-11-24 トヨタ自動車株式会社 燃料タンクシステム
JP5811890B2 (ja) * 2012-02-23 2015-11-11 トヨタ自動車株式会社 燃料タンクシステム
JP5807587B2 (ja) * 2012-02-24 2015-11-10 トヨタ自動車株式会社 燃料タンクシステム
JP6017167B2 (ja) * 2012-04-06 2016-10-26 愛三工業株式会社 トラップキャニスタ
EP2679430A1 (en) * 2012-06-27 2014-01-01 Caterpillar Inc. Fuel tanks for construction machines
JP2015137640A (ja) 2014-01-24 2015-07-30 京三電機株式会社 燃料蒸気制御弁およびそれを備える燃料蒸気処理装置
JP2016113965A (ja) * 2014-12-15 2016-06-23 京三電機株式会社 燃料蒸気システムの弁装置
FR3054609A1 (fr) * 2016-07-29 2018-02-02 Plastic Omnium Advanced Innovation & Res Regulateur de debit de ventilation pour un reservoir pressurise de vehicule.
WO2019042903A1 (en) 2017-08-29 2019-03-07 Plastic Omnium Advanced Innovation And Research SYSTEM AND METHOD FOR VARIATION OF THE OPENING SPEED OF A FUEL TANK VALVE
DE102017125283A1 (de) * 2017-10-27 2019-05-02 Alfmeier Präzision SE Ventilsystem für einen Kraftstofftank
CN108361433B (zh) * 2018-03-05 2024-06-14 皑壹汽车科技（上海）有限公司 一种用于汽车燃料箱的阀
US11299035B2 (en) * 2018-06-13 2022-04-12 Volvo Truck Corporation Flow regulation device, fuel managing system comprising such a device and automotive vehicle comprising such a system
DE102019119576A1 (de) * 2019-07-18 2021-01-21 Alfmeier Präzision SE Ventileinheit für einen Kraftstofftank
CN112324596A (zh) * 2020-10-22 2021-02-05 亚普汽车部件股份有限公司 电控阀及燃油系统
CN112594096A (zh) * 2020-12-09 2021-04-02 亚普汽车部件股份有限公司 一种电控阀、电控燃油系统及控制方法

Citations (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2576516A (en) * 1947-05-19 1951-11-27 Shand And Jurs Company Pressure relief valve
US3476146A (en) * 1967-02-10 1969-11-04 Dole Valve Co Anti-knock flow valve
GB2043301A (en) 1979-03-06 1980-10-01 Pegler Hattersley Ltd Radiator valves
US4308841A (en) * 1977-02-02 1982-01-05 General Motors Corporation Emission control system with integrated evaporative canister purge
JPS6062116A (ja) 1983-09-16 1985-04-10 Hitachi Ltd Ｘ線露光装置
JPH04124126A (ja) 1990-09-12 1992-04-24 Lion Corp 持続性カプセル剤
JPH04125377A (ja) 1990-09-14 1992-04-24 Matsushita Electric Works Ltd パイロット式電磁弁
US5143258A (en) * 1991-05-15 1992-09-01 Tokheim Corporation Pressure relief for vacuum operated valve
US5230625A (en) 1991-03-28 1993-07-27 Siemens Aktiengesellschaft Valve arrangement
US5497800A (en) 1993-11-05 1996-03-12 Toyoda Gosei Co., Ltd. Fuel vapor processing device
JPH08210530A (ja) 1995-02-03 1996-08-20 Toyota Motor Corp キャニスタ
US5687759A (en) * 1996-04-04 1997-11-18 The Curators Of The University Of Missouri Low operating power, fast-response servovalve
US5806553A (en) * 1995-07-17 1998-09-15 Sidwell; Herbert R. Fluid pressure control and relief apparatus
US6003499A (en) 1998-01-07 1999-12-21 Stant Manufacturing Inc. Tank vent control apparatus
JP2003049716A (ja) 2001-08-02 2003-02-21 Toyota Motor Corp 燃料タンクの給油燃料蒸気回収装置
US6601617B2 (en) 1999-05-28 2003-08-05 Borgwarner Inc. Electromechanical refueling control system
WO2005059359A1 (fr) 2003-12-15 2005-06-30 Shaochun Dou Appareil de levage de corps et dispositif de production d'energie
US6957663B2 (en) * 2002-04-26 2005-10-25 Tgk Co., Ltd. Solenoid control valve
JP2005308103A (ja) 2004-04-22 2005-11-04 Rinnai Corp パイロット弁
WO2006072633A1 (en) 2005-01-10 2006-07-13 Inergy Automotive Systems Research (Société Anonyme) Electronically controlled electromechanical valve
US20060150722A1 (en) 2005-01-12 2006-07-13 Denso Corporation Leak detector for evaporated fuel
WO2007088137A1 (en) * 2006-01-31 2007-08-09 Inergy Automotive Systems Research (Societe Anonyme) Method for recovering vapor during an onboard refueling operation
US20080083457A1 (en) * 2006-10-06 2008-04-10 Harley-Davidson Motor Company Group, Inc. Valve assembly for a motorcycle fuel tank
US7444997B2 (en) 2003-12-15 2008-11-04 Inergy Automotive Systems Research (Societe Anonyme) Electronically controlled electromechanical valve

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6062116U (ja) * 1983-10-04 1985-05-01 株式会社　京浜精機製作所 流量制御弁
JP3090598B2 (ja) * 1994-12-15 2000-09-25 エヌオーケー株式会社 フューエルタンクの燃料蒸気処理装置
JPH10205634A (ja) * 1997-01-17 1998-08-04 Nok Corp 液体遮断弁装置
US20030140970A1 (en) * 2002-01-31 2003-07-31 Benjey Robert P. Method and system for controlling liquid fuel and vapor flow during refueling of a motor vehicle fuel tank
US20040194831A1 (en) * 2003-04-01 2004-10-07 Balsdon David W. System and method including a fluid actuated fuel tank isolation valve
JP4487776B2 (ja) * 2005-01-06 2010-06-23 株式会社デンソー 燃料供給制御装置
US20070000542A1 (en) * 2005-06-30 2007-01-04 Ti Group Automotive Systems, L.L.C. Fuel tank valve
JP2007138815A (ja) * 2005-11-17 2007-06-07 Suzuki Motor Corp 船舶内設置型燃料タンクの蒸発燃料処理装置

Patent Citations (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2576516A (en) * 1947-05-19 1951-11-27 Shand And Jurs Company Pressure relief valve
US3476146A (en) * 1967-02-10 1969-11-04 Dole Valve Co Anti-knock flow valve
US4308841A (en) * 1977-02-02 1982-01-05 General Motors Corporation Emission control system with integrated evaporative canister purge
GB2043301A (en) 1979-03-06 1980-10-01 Pegler Hattersley Ltd Radiator valves
JPS6062116A (ja) 1983-09-16 1985-04-10 Hitachi Ltd Ｘ線露光装置
JPH04124126A (ja) 1990-09-12 1992-04-24 Lion Corp 持続性カプセル剤
JPH04125377A (ja) 1990-09-14 1992-04-24 Matsushita Electric Works Ltd パイロット式電磁弁
US5230625A (en) 1991-03-28 1993-07-27 Siemens Aktiengesellschaft Valve arrangement
US5143258A (en) * 1991-05-15 1992-09-01 Tokheim Corporation Pressure relief for vacuum operated valve
US5497800A (en) 1993-11-05 1996-03-12 Toyoda Gosei Co., Ltd. Fuel vapor processing device
JPH08210530A (ja) 1995-02-03 1996-08-20 Toyota Motor Corp キャニスタ
US5806553A (en) * 1995-07-17 1998-09-15 Sidwell; Herbert R. Fluid pressure control and relief apparatus
US5687759A (en) * 1996-04-04 1997-11-18 The Curators Of The University Of Missouri Low operating power, fast-response servovalve
US6003499A (en) 1998-01-07 1999-12-21 Stant Manufacturing Inc. Tank vent control apparatus
US6601617B2 (en) 1999-05-28 2003-08-05 Borgwarner Inc. Electromechanical refueling control system
JP2003049716A (ja) 2001-08-02 2003-02-21 Toyota Motor Corp 燃料タンクの給油燃料蒸気回収装置
US6957663B2 (en) * 2002-04-26 2005-10-25 Tgk Co., Ltd. Solenoid control valve
US7444997B2 (en) 2003-12-15 2008-11-04 Inergy Automotive Systems Research (Societe Anonyme) Electronically controlled electromechanical valve
WO2005059359A1 (fr) 2003-12-15 2005-06-30 Shaochun Dou Appareil de levage de corps et dispositif de production d'energie
JP2005308103A (ja) 2004-04-22 2005-11-04 Rinnai Corp パイロット弁
WO2006072633A1 (en) 2005-01-10 2006-07-13 Inergy Automotive Systems Research (Société Anonyme) Electronically controlled electromechanical valve
US20060150722A1 (en) 2005-01-12 2006-07-13 Denso Corporation Leak detector for evaporated fuel
WO2007088137A1 (en) * 2006-01-31 2007-08-09 Inergy Automotive Systems Research (Societe Anonyme) Method for recovering vapor during an onboard refueling operation
US7882824B2 (en) * 2006-01-31 2011-02-08 Inergy Automotive Systems Research (S.A) Method for recovering vapor during an onboard refueling operation
US20080083457A1 (en) * 2006-10-06 2008-04-10 Harley-Davidson Motor Company Group, Inc. Valve assembly for a motorcycle fuel tank

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170253116A1 (en) * 2012-12-24 2017-09-07 Eaton Corporation Valve assembly for a tank of a vehicle and a method of creating a vacuum in the tank

Also Published As

Publication number Publication date
AU2009286409A1 (en) 2010-03-04
CN102165174B (zh) 2015-04-22
MX2011002245A (es) 2011-04-05
RU2011111497A (ru) 2012-10-10
EP2321518B1 (en) 2017-09-20
WO2010023534A1 (en) 2010-03-04
US20100051116A1 (en) 2010-03-04
KR20110053369A (ko) 2011-05-20
JP2015061779A (ja) 2015-04-02
KR101602981B1 (ko) 2016-03-11
EP2321518A1 (en) 2011-05-18
JP5859094B2 (ja) 2016-02-10
CN102165174A (zh) 2011-08-24
JP2012500750A (ja) 2012-01-12

Similar Documents

Publication Publication Date Title
US8931508B2 (en) Piloted fuel tank vapor isolation valve
US7107971B2 (en) Isolation valve useful in fuel tank emission control systems
US20140137964A1 (en) Fuel tank system
CA2541756C (en) Vehicle evaporative system diagnostic
JP6287809B2 (ja) 燃料タンクシステム
JP5817536B2 (ja) 燃料タンクシステム
US9683522B2 (en) Fuel tank system and method for sensing perforation
CN111033025B (zh) 用于改变燃料储箱阀门打开速度的系统和方法
JPH06183271A (ja) 燃料タンクのベントカットバルブ
JP5724883B2 (ja) 燃料タンクシステム
JP3531300B2 (ja) 燃料蒸気排出制御装置
JP3551577B2 (ja) 圧力制御弁および燃料蒸気圧力制御装置
JP5849755B2 (ja) 燃料タンクシステム
JP2013167177A (ja) 燃料タンクシステム
JPH08276757A (ja) 蒸発燃料排出防止装置
KR20030047356A (ko) 자동차용 연료 시스템
JPWO2013018215A1 (ja) 燃料タンクシステム

Legal Events

Date Code Title Description
AS Assignment

Owner name: EATON CORPORATION,OHIO

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MARTIN, CHARLES J.;ERDMANN, MATTHEW L.;OSTROSKY, JAMES P.;SIGNING DATES FROM 20090810 TO 20090817;REEL/FRAME:023106/0212

Owner name: EATON CORPORATION, OHIO

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MARTIN, CHARLES J.;ERDMANN, MATTHEW L.;OSTROSKY, JAMES P.;SIGNING DATES FROM 20090810 TO 20090817;REEL/FRAME:023106/0212

STCF Information on status: patent grant

Free format text: PATENTED CASE

MAFP Maintenance fee payment

Free format text: PAYMENT OF MAINTENANCE FEE, 4TH YEAR, LARGE ENTITY (ORIGINAL EVENT CODE: M1551)

Year of fee payment: 4

FEPP Fee payment procedure

Free format text: MAINTENANCE FEE REMINDER MAILED (ORIGINAL EVENT CODE: REM.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

LAPS Lapse for failure to pay maintenance fees

Free format text: PATENT EXPIRED FOR FAILURE TO PAY MAINTENANCE FEES (ORIGINAL EVENT CODE: EXP.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

STCH Information on status: patent discontinuation

Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362

FP Lapsed due to failure to pay maintenance fee

Effective date: 20230113